SPACE 2026 — IEEE SPace, Aerospace and defenCE Conference

Control Under Uncertainty — From Trajectory Optimization to Adaptive Control

Control Under Uncertainty — From Trajectory Optimization to Adaptive Control

July 19, 2026 • 4 hours

Session Organizers

Dr. Maruthi Akella

Professor, Aerospace Engineering and Engineering Mechanics, University of Texas at Austin

Dr. Roshan Eapen

Assistant Professor, Aerospace Engineering, Pennsylvania State Universityr

Dr. Puneet Singla

Harry and Arlene Schell Professor of the Aerospace engineering, Pennsylvania State University

Abstract

Future aerospace missions increasingly operate in environments where nonlinear dynamics, tight performance constraints, and uncertainty are central design drivers. This workshop presents a unified framework for control under uncertainty, with direct application to spacecraft operating in cislunar space, close-proximity and formation missions, and hypersonic vehicles subject to severe state and control constraints.

In cislunar space, spacecraft motion is governed by multi-body gravitational dynamics that exhibit sensitive dependence on initial conditions and long-horizon instability. Trajectory design in this regime requires sophisticated numerical methods, while feedback stabilization near libration point orbits demands control laws that respect nonlinear structure and limited actuation. Uncertainty in ephemerides, environmental disturbances, and model mismatch further complicate mission design. Close-proximity operations introduce additional layers of complexity. Rendezvous, docking, on-orbit servicing, and formation flying must satisfy strict safety constraints, including collision avoidance, plume impingement limits, line-of-sight requirements, and actuator saturation. These missions demand trajectory planning methods that rigorously handle state and control constraints while maintaining robustness to estimation and modeling errors. Hypersonic vehicles present a different but equally challenging regime. Strong aerodynamic coupling, rapidly varying atmospheric conditions, thermal constraints, and limited control authority create tightly constrained, highly nonlinear control problems. Robust guidance and control architectures must account for parametric uncertainty, unmodeled dynamics, and state-dependent performance limitations.

This workshop develops unified perspectives that bridge trajectory optimization, nonlinear feedback design, stochastic optimal control, and adaptive control methodologies. Emphasis is placed on understanding how structure in optimal control problems including Hamiltonian formulations and value function geometry can be leveraged to design computationally tractable, robust controllers for safety-critical aerospace applications. By integrating numerical optimal control, dynamical systems theory, stochastic control, and adaptive methods, the session provides participants with conceptual and computational tools for addressing uncertainty within advanced aerospace vehicle guidance and control problems. At the end of the tutorial session, participants will be able to:

  1. Formulate constrained nonlinear optimal control problems arising in cislunar spacecraft missions, proximity operations, and hypersonic flight.
  2. Connect dynamical systems concepts and Hamilton–Jacobi theory to the synthesis of nonlinear feedback control policies.
  3. Evaluate and design control strategies that explicitly account for parametric and non-parametric uncertainty using stochastic and adaptive control methods.
  4. Integrate open-loop trajectory optimization with robust feedback design in safety-critical aerospace applications involving state and actuator constraints.

Abstracts for Talks:

Numerical Methods for Trajectory Planning: (Speaker: Maruthi Akella and Puneet Singla)
The session will begin with fundamental principles of indirect optimal control, emphasizing state-of-the-art numerical techniques for solving two-point boundary value problems. Both classical formulations and modern computational strategies will be discussed, with attention to practical implementation challenges. The application of these methods to design ballistic trajectories for space vehicles in multi-body environment and trajectory planning for high-speed vehicles under state and control constraints will be demonstrated.

Dynamic System Theory for Optimal Feedback Control (Speaker: Roshan Eapen)
This session will explore the deep connections between dynamical systems theory and optimal feedback control. Leveraging Hamilton–Jacobi theory, we will examine how optimal control policies emerge from canonical transformations and discuss implications for nonlinear model predictive control.

Adaptive Control (Speaker: Maruthi Akella)
This Session will address control under uncertainty, covering both stochastic optimal control and adaptive control methodologies. Approaches for handling parametric and non-parametric uncertainty will be presented, along with insights into robustness and learning-based adaptation.

Speaker Biographies

Dr. Maruthi Akella

Dr. Maruthi Akella is a professor in Aerospace Engineering and Engineering Mechanics at UT Austin where he holds the Cockrell Family Endowed Chair in Engineering. He is founding director for the Center for Autonomous Air Mobility and faculty lead coordinator for the controls, autonomy, and robotics area at UT Austin. His research encompasses coordinated systems, learning, adaptation, and vision-based sensing. His research group contributed for the onboard guidance algorithm for the Intuitive Machines IM-1 mission – the first U.S. moon landing in more than 50 years since the Apollo era. The major impacts of Dr. Akella’s work have been recognized through the AIAA Mechanics and Control of Flight Award, the AAS Dirk Brouwer Award, the IEEE-CSS Award for Excellence in Aerospace Control, and the Judith Resnik Space Award from the IEEE Aerospace and Electronic Systems Society. Dr. Akella is Editor-in-Chief for the Journal of the Astronautical Sciences and a Fellow of the AIAA, IEEE, and AAS. In October 2024, the International Astronomical Union designated asteroid number 5376 – a nearly 5-mile diameter-sized minor planet from the main asteroid belt – as “Maruthiakella” honoring Dr. Akella’s contributions to “many successful applications in astrodynamics.”

Dr. Roshan Eapen

Dr. Roshan Eapen is an assistant Professor of Aerospace Engineering at the Pennsylvania State University. His research interest lies at the intersection of Dynamical Systems Theory, Astrodynamics, and Computational Vision with specific focus on semi-analytic satellite orbit and attitude theories, optimal control of spacecraft, sensor modeling, light-matter interaction, and vision-based navigation. He runs the Computational Astrodynamics Research and Experiments (CARE) lab which host the Penn State University Dynamial observatory (PSUDO), a 0.6m telescope observatory and ground station. He is a JN Tata scholar (2015) and the recipient of the Heep Graduate Fellowship from the Hagler Institute of Advanced Studies.

Dr. Puneet Singla

Dr. Puneet Singla is the Harry and Arlene Schell Professor of the Aerospace engineering at the Pennsylvania State University (PSU). Dr. Singla’s research interface nonlinear dynamics with approximation theory, sensing, uncertainty analysis, and optimal control. He significantly advanced data-driven approaches for a diverse range of highly complex problems such as space domain awareness (SDA), guidance navigation and control (GNC) of hypersonic vehicles, and accurate prediction of toxic plume dispersions. His research related honors include the IEEE AESS’s Judith A. Resnik Award, NSF CAREER award, the AFOSR Young Investigator award, the Penn State Engineering Alumni Outstanding Researcher Award, the University at Buffalo’s “Exceptional Scholar” Young Investigator Award and the Texas A&M University’s Young Aerospace Engineering Distinguished Alumni Award in recognition of his scholarly activities. He is IEEE AESS’s distinguished lecturer since 2024. He is a fellow of American Astronautical Society (AAS) and American Institute of Aeronautics and Astronautics (AIAA).

Format & Duration

This tutorial session will be approximately 4 hours in duration. The workshop is structured into a single session comprising multiple key topics: Numerical methods for trajectory planning, optimal feedback control, optimal stochastic control and adaptive control. The first major talk, Numerical Methods for Trajectory Planning, will cover fundamental aspects of the indirect optimal control and state-of-the-art methods for solving two-point boundary value problems. This will be followed by Dynamic System Theory for Optimal Feedback Control, which will focus on the connections between dynamical system theory and optimal feedback control while leveraging the Hamilton Jacobi theory to solve for optimal control policy. The third talk, Adaptive Control will address key methodologies for control under parametric and non-parametric uncertainty. The session will conclude with a discussion segment, allowing participants to engage with the speakers, ask questions, and explore practical implications of the presented topics.

Target Audience

Practitioners looking for advanced techniques in trajectory planning, guidance and control for aerospace vehicles. Researchers looking for new ideas and the connection between theory and practice; students and early career professionals looking for better understanding of the foundation of optimal control theory and the development of optimal guidance strategies; Defense space professionals focused on control of high speed vehicles under memory and computational constraints will gain insights into operational challenges like how to accommodate different kind of uncertainties while designing optimal control policy.

Target Audience

Time (Minutes) Session / Topic
10 minutes Introduction and Opening Remarks
90 minutes Numerical Methods for Trajectory Planning
90 minutes Dynamic System Theory for Optimal Feedback Control (90 minutes)k
—————————–Break—————————–
60 minutes Adaptive Control
20 minutes Discussion and Audience Interaction